Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels (2022)
Source: Composite Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA
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CABRAL, Myrella Vieira e MARQUES, Flavio Donizeti e FERREIRA, Antonio J. M. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels. Composite Structures, v. 286, p. 1-15, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2021.115128. Acesso em: 29 set. 2024.APA
Cabral, M. V., Marques, F. D., & Ferreira, A. J. M. (2022). Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels. Composite Structures, 286, 1-15. doi:10.1016/j.compstruct.2021.115128NLM
Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels [Internet]. Composite Structures. 2022 ; 286 1-15.[citado 2024 set. 29 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128Vancouver
Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels [Internet]. Composite Structures. 2022 ; 286 1-15.[citado 2024 set. 29 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128